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公开(公告)号：US06176024B1
公开(公告)日：2001-01-23
申请号：US09526820
申请日：2000-03-16
IPC分类号： F26B1900
CPC分类号： F26B21/004 , B60S3/002
摘要： A plurality of bags (16), each of a substantially rectangular cross-section defined by spaced and parallel bag panels (18) interconnected by shorter sides (20), have inlets respectively connected to a support plenum (12) and extend to a distal end (22). An elongated nozzle (24) extends across each bag (16) at the distal end (22) between the sides (20) and converges from the bag panels (18) to a nozzle opening (26) for directing air toward the object. The assembly is characterized by a plurality of nozzle gussets (32) each including two layers (34) of flexible material suspended between the first and second nozzle panels (30) for bulging away from one another and toward the next adjacent nozzle gusset. Consequently, the spaced layers (34) of next adjacent nozzle gussets (32) bulge toward one another in response to air flow through the nozzle (24) to create a restriction and increased velocity of the air flow.
摘要翻译： 多个袋（16），每个由通过较短侧（20）互连的间隔开且平行的袋板（18）限定的基本上矩形的横截面分别连接到支撑室（12）并延伸到远端 结束（22）。 细长的喷嘴（24）在侧面（20）之间的远端（22）处跨越每个袋（16）延伸并且从袋面板（18）到用于将空气引向物体的喷嘴开口（26）会聚。 组件的特征在于多个喷嘴角撑板（32），每个喷嘴角撑板（32）均包括悬挂在第一和第二喷嘴面板（30）之间的两层柔性材料层（34），用于彼此远离并朝着下一个相邻的喷嘴角撑板凸出。 因此，响应于通过喷嘴（24）的空气流动，下一个相邻喷嘴角撑板（32）的间隔开的层（34）朝向彼此凸出，以产生限制并增加气流的速度。
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公开(公告)号：US5901461A
公开(公告)日：1999-05-11
申请号：US53926
申请日：1998-04-02
CPC分类号： B60S3/002
摘要： An assembly for blowing liquids from the surfaces of a vehicle comprising support plenum (10) for distributing a stream of air to the surfaces of a vehicle, a blower (16) connected to said support plenum (10) for producing the stream of air, and an overhead bag (18) extending downwardly from the plenum (10) to a distal end. A nozzle is disposed at the distal end and includes a center section (20) having a length (Y) extending horizontally between ends for directing air against the top of a vehicle. The nozzle is characterized by including an inwardly directed end section (22) at each end of the center section (20) to define outward tips (24) of the nozzle for directing air downwardly and inwardly against the sides of a vehicle. A positioner (30) positions the vehicle to combine with the geometric configuration of the overhead bag (18) to assure that the stream of air emitted from the nozzle tips (24) impacts the sides of the vehicle.
摘要翻译： 一种用于从车辆表面吹出液体的组件，包括用于将空气流分配到车辆表面的支撑气室（10），连接到所述支撑气室（10）的用于产生空气流的鼓风机（16） 以及从充气室（10）向下延伸到远端的顶棚袋（18）。 喷嘴设置在远端处，并且包括具有在端部之间水平延伸的长度（Y）的中心部分（20），用于将空气引导到车辆的顶部。 喷嘴的特征在于在中心部分（20）的每个端部处包括向内指向的端部部分（22），以限定喷嘴的向外的尖端（24），用于将空气向下和向内引导抵靠车辆的侧面。 定位器（30）将车辆定位成与顶棚袋（18）的几何构型组合，以确保从喷嘴尖端（24）发射的空气流冲击车辆的侧面。
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公开(公告)号：US06745497B2
公开(公告)日：2004-06-08
申请号：US10280914
申请日：2002-10-25
IPC分类号： F26B1900
CPC分类号： B60S3/002
摘要： An axle (30) supports both a nozzle plenum (18) and a plurality lower tubes (28) that telescope into a plurality of upper tubes (26). The nozzle plenum (18) is moved vertically up and down between various operating positions as the tubes (26, 28) telescope into and out of one another to accommodate the changing longitudinal configuration of a vehicle and the nozzle plenum (18) may be rotated about the axle (30) to efficiently direct air against the contour of the vehicle.
摘要翻译： 轴（30）支撑喷嘴增压室（18）和望远成多个上管（26）的多个下管（28）。 当管（26,28）望远镜彼此伸入和移出时，喷嘴增压室（18）在不同的操作位置之间垂直上下移动，以适应车辆的变化的纵向结构，并且喷嘴增压室（18）可以旋转 围绕所述轴（30）有效地将空气对准所述车辆的轮廓。
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公开(公告)号：US07284296B2
公开(公告)日：2007-10-23
申请号：US10792049
申请日：2004-03-03
IPC分类号： F26B21/00
CPC分类号： B60S3/002 , F04D27/003
摘要： A valve plate (54) is slidably moved on a frame (52) by an actuator (62) between open and closed positions to control the supply of air sucked into the inlet (44) of a blower system (40) that supplies pressurized air through an outlet (46) to a plenum (12) for distribution to said nozzle (16, 18). By disposing the valve plate (54) at the inlet, the blower motor (49) may run continuously without a load as the impeller is not pumping air when there is no demand to blow the water from a vehicle.
摘要翻译： 阀板（54）通过致动器（62）在打开和关闭位置之间在框架（52）上可滑动地移动，以控制吸入到供应加压空气的鼓风机系统（40）的入口（44）中的空气的供应 通过出口（46）到通气室（12）以分配到所述喷嘴（16,18）。 通过将阀板（54）设置在入口处，当不需要从车辆吹出水时，鼓风机马达（49）可以连续地运行而没有负载，因为叶轮不泵送空气。
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公开(公告)号：US6038781A
公开(公告)日：2000-03-21
申请号：US268959
申请日：1999-03-16
CPC分类号： B64F5/0054 , B64F5/0063
摘要： The assembly includes a plurality of flexible and inflatable bags 43, 44, 45, 46, 47, 48, 56 and 58, each having a rectangular cross section with an open end for receiving air from various ducts 30, 32, 34, 36, 38, 40, 62 and 66, and extending vertically to a nozzle end 52. A plurality of first starboard bags 43 overlap a plurality of second starboard bags 44 in the horizontal direction and a plurality of first port bags 46 overlap a plurality of second port bags 47 in the horizontal direction. Also, the second starboard 44 and port 47 bags are spaced downstream from the first 43 starboard and port 46 bags. The nozzles 52 of the first starboard bags 43 are disposed in a first horizontal V.sub.a. -shape in relationship with the first port bags 46 to direct the emitting air in the emitting planes rearwardly and outwardly on each side of the aircraft 10 to move deicing material outwardly and rearwardly over the wings 12 and 14 and the nozzles 52 of the second starboard 44 and port 47 bags are disposed in a second horizontal V.sub.b -shape with each other to direct the emitting air in the emitting planes rearwardly and outwardly from the aircraft 10 to move deicing material outwardly and rearwardly over the wings from the first starboard 43 and port 46 bags. Three third starboard bags 45 are aligned horizontally with three third port bags 48 and downstream of the second starboard 44 and port 47 bags. A plurality of starboard 56 and port 58 are disposed close together for removing deicing material from the horizontal stabilizer of the aircraft.
摘要翻译： 组件包括多个柔性和可充气的袋子43,44,45,46,47,48,56和58，每个袋子具有矩形横截面，开口端用于从各种管道30,32,34,36,36接收空气， 38,40,62和66，并且垂直地延伸到喷嘴端52.多个第一右舷行李箱43在水平方向上与多个第二右舷行李箱44重叠，并且多个第一口袋46与多个第二端口 袋47在水平方向。 此外，第二右舷44和47口袋与第一个43右舷和46个行李箱的下游隔开。 第一右舷行李箱43的喷嘴52与第一端口袋46相关地设置成第一水平的Va.形状，以便在飞机10的每一侧向后和向外引导发射平面中的排放空气，以移动除冰材料 向上和向后在翼12和14之上，并且第二右舷44和端口47的喷嘴52袋彼此相邻地设置成第二水平的Vb形状，以将飞行器10的向后和向外的发射平面中的排出空气引导 以从第一右舷43和46口袋向外和向后移动除冰材料。 三个第三右舷行李箱45与三个第三口袋48水平对准，第二右舷44和47个袋子的下游。 多个右舷56和端口58靠近放置，用于从飞机的水平稳定器上除去除冰材料。
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公开(公告)号：US5960564A
公开(公告)日：1999-10-05
申请号：US32069
申请日：1998-02-27
CPC分类号： B60S3/002
摘要： An assembly for blowing liquids from a vehicle in a car wash which is characterized by the pair of first 24 and second 26 side bags extending from each of side supports 14, 16, 114 and 116 with each pair 24 and 26 of side bags being coextensive and extending vertically along the associated side support 14, 16, 114 or 116 and outwardly therefrom to elongated generally vertical nozzles 32. The first side bag 24 is disposed to direct the output flow therefrom along a first plane (A) directed forwardly twenty degrees (20.degree.) and the second side bag 26 is disposed to direct the output flow therefrom along a second plane (B) directed rearwardly twenty degrees (20.degree.).
摘要翻译： 一种用于在洗车中从车辆吹出液体的组件，其特征在于，从侧面支撑件14,16,114和116中的每一个延伸的一对第一24和第二侧边袋124，每个侧袋24和26是共延伸的 并且沿着相关联的侧支撑件14,16,114或116垂直延伸并从其向外延伸到细长的大致垂直的喷嘴32.第一侧袋24设置成沿着朝向前方20度的第一平面（A）引导其输出流， 20度），并且第二侧袋26设置成沿着朝向20度（20度）的第二平面（B）引导其输出流。
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公开(公告)号：US06519872B2
公开(公告)日：2003-02-18
申请号：US09849165
申请日：2001-05-04
IPC分类号： F26B1900
CPC分类号： B60S3/002
摘要： A plurality of pairs of telescoping tubes (20) and (22) interconnect a support plenum (12) and a nozzle system (14) for delivering air from the plenum (12) to the nozzle system (14) while allowing the nozzle system (14) to move in an adjustment direction toward and away from the plenum (12). The nozzle system (14) is elongated and includes a fixed shell (24) and a movable shell (26) movably supported by the fixed shell (24). The assembly (10) is characterized by actuators (42) for moving the nozzle system (14) between the various vertical-operating positions and a motor (46) for rotating the nozzle (16). The nozzle system (14) may be moved up and down to accommodate the changing longitudinal configuration of the vehicle (18) and the nozzle (16) may be rotated about the nozzle axis to efficiently direct air against the contour of the vehicle (18).
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公开(公告)号：US5950324A
公开(公告)日：1999-09-14
申请号：US25061
申请日：1998-02-17
CPC分类号： B64F5/0054 , B64F5/0063
摘要： The assembly includes a plurality of flexible and inflatable bags 43, 44, 45, 46, 47, 48, 56 and 58, each having a rectangular cross section with an open end for receiving air from various ducts 30, 32, 34, 36, 38, 40, 62 and 66, and extending vertically to a nozzle end 52. A plurality of first starboard bags 43 overlap a plurality of second starboard bags 44 in the horizontal direction and a plurality of first port bags 46 overlap a plurality of second port bags 47 in the horizontal direction. Also, the second starboard 44 and port 47 bags are spaced downstream from the first 43 starboard and port 46 bags. The nozzles 52 of the first starboard bags 43 are disposed in a first horizontal V.sub.a. -shape in relationship with the first port bags 46 to direct the emitting air in the emitting planes rearwardly and outwardly on each side of the aircraft 10 to move deicing material outwardly and rearwardly over the wings 12 and 14 and the nozzles 52 of the second starboard 44 and port 47 bags are disposed in a second horizontal V.sub.b -shape with each other to direct the emitting air in the emitting planes rearwardly and outwardly from the aircraft 10 to move deicing material outwardly and rearwardly over the wings from the first starboard 43 and port 46 bags. Three third starboard bags 45 are aligned horizontally with three third port bags 48 and downstream of the second starboard 44 and port 47 bags. A plurality of starboard 56 and port 58 are disposed close together for removing deicing material from the horizontal stabilizer of the aircraft.
摘要翻译： 组件包括多个柔性和可充气的袋子43,44,45,46,47,48,56和58，每个袋子具有矩形横截面，开口端用于从各种管道30,32,34,36,36接收空气， 38,40,62和66，并且垂直地延伸到喷嘴端52.多个第一右舷行李箱43在水平方向上与多个第二右舷行李箱44重叠，并且多个第一口袋46与多个第二端口 袋47在水平方向。 此外，第二右舷44和47口袋与第一个43右舷和46个行李箱的下游隔开。 第一右舷行李箱43的喷嘴52与第一端口袋46相关地设置成第一水平的Va.形状，以便在飞机10的每一侧向后和向外引导发射平面中的排放空气，以移动除冰材料 向上和向后在翼12和14之上，并且第二右舷44和端口47的喷嘴52袋彼此相邻地设置成第二水平的Vb形状，以将飞行器10的向后和向外的发射平面中的排出空气引导 以从第一右舷43和46口袋向外和向后移动除冰材料。 三个第三右舷行李箱45与三个第三口袋48水平对准，第二右舷44和47个袋子的下游。 多个右舷56和端口58靠近放置，用于从飞机的水平稳定器上除去除冰材料。
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